Research Catalog

Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7

Title
Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7 [microform] / Don E. Avery.
Author
Avery, Don E.
Publication
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.

Details

Additional Authors
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Description
1 v.
Series Statement
NASA technical paper ; 2307
Subject
  • Cold surfaces
  • Heat shielding
  • Hypersonic flow
  • Impingement
  • Reusable heat shielding
  • Thermal protection
  • Tiles
  • Turbulent boundary layer
  • Turbulent flow
Note
  • "August 1985"--Cover.
Reproduction (note)
  • Microfiche.
Call Number
GPO Microfiche NAS 1.60:2307
OCLC
marcive56779515
Author
Avery, Don E.
Title
Experimental aerodynamic heating to simulated space shuttle tiles in laminar and turbulent boundary layers with variable flow angles at a nominal Mach number of 7 [microform] / Don E. Avery.
Imprint
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985.
Series
NASA technical paper ; 2307
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1985] 1 microfiche.
Added Author
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Gpo Item No.
0830-H-15 (MF)
Sudoc No.
NAS 1.60:2307
Research Call Number
GPO Microfiche NAS 1.60:2307
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